EP3057779A1 - Procédé de production d'un élément structural composite renforcé par des fibres - Google Patents
Procédé de production d'un élément structural composite renforcé par des fibresInfo
- Publication number
- EP3057779A1 EP3057779A1 EP14783801.5A EP14783801A EP3057779A1 EP 3057779 A1 EP3057779 A1 EP 3057779A1 EP 14783801 A EP14783801 A EP 14783801A EP 3057779 A1 EP3057779 A1 EP 3057779A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- core element
- fiber composite
- composite component
- reinforced
- profile
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000000835 fiber Substances 0.000 title claims abstract description 51
- 239000002131 composite material Substances 0.000 title claims abstract description 36
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 8
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 34
- 238000009954 braiding Methods 0.000 claims abstract description 7
- 239000011159 matrix material Substances 0.000 claims abstract description 7
- 238000000034 method Methods 0.000 claims description 12
- 239000004033 plastic Substances 0.000 claims description 11
- 238000005470 impregnation Methods 0.000 claims description 10
- 229920003023 plastic Polymers 0.000 claims description 10
- 239000000463 material Substances 0.000 claims description 9
- 230000002787 reinforcement Effects 0.000 claims description 9
- 239000002184 metal Substances 0.000 claims description 6
- 239000004917 carbon fiber Substances 0.000 claims description 5
- 238000005187 foaming Methods 0.000 claims description 5
- 239000003365 glass fiber Substances 0.000 claims description 5
- 239000011347 resin Substances 0.000 claims description 5
- 229920005989 resin Polymers 0.000 claims description 5
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 239000004760 aramid Substances 0.000 claims description 3
- 229920006231 aramid fiber Polymers 0.000 claims description 3
- 239000002984 plastic foam Substances 0.000 claims description 3
- 238000001721 transfer moulding Methods 0.000 claims description 3
- 239000006260 foam Substances 0.000 claims description 2
- 239000006262 metallic foam Substances 0.000 claims description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 2
- 239000003677 Sheet moulding compound Substances 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000011151 fibre-reinforced plastic Substances 0.000 description 2
- 239000006261 foam material Substances 0.000 description 2
- 238000001746 injection moulding Methods 0.000 description 2
- 239000002023 wood Substances 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 239000011265 semifinished product Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 239000001993 wax Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
- B29C44/20—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of indefinite length
- B29C44/32—Incorporating or moulding on preformed parts, e.g. linings, inserts or reinforcements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
- B29C70/021—Combinations of fibrous reinforcement and non-fibrous material
- B29C70/023—Combinations of fibrous reinforcement and non-fibrous material with reinforcing inserts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
- B29C70/222—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
- B29C70/865—Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04C—BRAIDING OR MANUFACTURE OF LACE, INCLUDING BOBBIN-NET OR CARBONISED LACE; BRAIDING MACHINES; BRAID; LACE
- D04C1/00—Braid or lace, e.g. pillow-lace; Processes for the manufacture thereof
- D04C1/02—Braid or lace, e.g. pillow-lace; Processes for the manufacture thereof made from particular materials
-
- D—TEXTILES; PAPER
- D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
- D04C—BRAIDING OR MANUFACTURE OF LACE, INCLUDING BOBBIN-NET OR CARBONISED LACE; BRAIDING MACHINES; BRAID; LACE
- D04C3/00—Braiding or lacing machines
- D04C3/48—Auxiliary devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/04—Condition, form or state of moulded material or of the material to be shaped cellular or porous
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
- B29K2105/10—Cords, strands or rovings, e.g. oriented cords, strands or rovings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3002—Superstructures characterized by combining metal and plastics, i.e. hybrid parts
-
- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2505/00—Industrial
- D10B2505/02—Reinforcing materials; Prepregs
Definitions
- the invention relates to a method for producing a reinforced fiber composite component and a reinforced fiber composite component.
- Fiber composite components find increasing use in motor vehicles, since they have a high rigidity and low weight compared to corresponding components made of pure, metallic material.
- fiber composite components which comprise a support core, which is coated with a fiber structure of carbon or glass fibers by wrapping or braiding. It is provided in this way a hollow profile-shaped fiber structure whose dimensional stability is supported by the arranged inside the hollow profile formed support core and thus strengthened.
- support cores made of plastic foam, wax, wood, or metal application.
- the object of the invention is to provide a particularly stable and break-through fiber composite component with the lowest possible weight.
- a reinforcing profile and this enclosed with a core element.
- the core element is applied, for example, on an outer surface of the reinforcing profile and thus surrounds the reinforcing profile at least in a circumferential direction of the reinforcing profile.
- the core element reinforced by the reinforcing profile and depending on the choice of material, a change in the material properties of the entire fiber composite component is effected, so that a break at high loads is prevented.
- the reinforcing profile can comprise a rod-shaped or tubular profile made of plastic and / or metal and / or fiber-reinforced material, in particular fiber-reinforced plastic or fiber-reinforced metal.
- the profile may have any cross-sectional shape which is extended in a longitudinal direction of the profile.
- the simplest example of this is a circular cross-section which extends to a hollow cylinder or tubular in the longitudinal direction. It goes without saying that others as well
- Cross-sectional shapes can be selected, in particular ovals or polygonal cross sections can be used.
- the reinforcing profile can be designed as a hollow profile (for example tubular) or as a solid profile made of solid material (for example rod-shaped).
- the construction of the fiber composite component allows the cross section of the reinforcing profile to be carried out independently of a geometry of the shell or of the outer contour of the fiber composite component.
- the cross section of the reinforcing profile can be executed weight, load and / or power optimized. It is also possible to design the cross-sectional shape constant or varying along a longitudinal extent of the reinforcing profile.
- the core member may be applied to the outer surface of the reinforcing profile and follow its outer contour, an outer surface or contour of the core member may have a cross-sectional shape different from the reinforcing profile. This can be oriented, for example, to a contour of the entire fiber composite component, so that after the production of the sheathing or the impregnation, the desired component contour is provided.
- the core element thus bridges a possible geometry jump or geometry difference between the reinforcement part and the sheathing or the component contour.
- An exemplary embodiment is shown in FIG.
- the step of impregnation may in particular include impregnation by means of the resin transfer molding process (abbreviated RTM). It is also possible, the step of impregnation by means of other known
- Impregnation already known, so that can be dispensed with their detailed description.
- the sheath may comprise, for example, continuous fibers of glass fibers, aramid fibers and / or carbon fibers.
- the sheath is to be understood as a fiber structure, which is produced in particular by braiding and impregnated with a matrix.
- the materials of the continuous fibers can be arbitrarily combined with different materials of the core element.
- the core element is a suitable connectivity on the one hand with the reinforcing profile, and on the other hand with the sheath 'crucial.
- the core member should preferably have sufficient pressure stability to withstand, for example, injection of matrix during the impregnation step.
- the core element may be configured, for example, as a plastic element, as a wood element or as a foam element made of metal or plastic foam.
- a plastic element for example, it is possible to produce the plastic element by means of known injection molding.
- an additional reinforcement of the plastic element with fibers, such as carbon fibers, glass fibers or aramid fibers is possible.
- the plastic element can be designed as SMC (Sheet Molding Compound) or the like.
- Particularly suitable as a matrix are plastics or resins which are introduced into the core element and hardened, at least into the fiber structure of the sheath, by the step of impregnation, or additionally-as far as possible-in the core element. In this way, at least the impregnated Um- Sheath made of fiber-reinforced plastic or fiber reinforced resin formed.
- the step of enclosing the reinforcing profile may comprise foaming or overmolding for producing the enclosing core element.
- the reinforcing profile can be inserted into a corresponding foaming tool or injection molding tool.
- a reinforced fiber composite component with a core element is proposed, which is braided with a sheath, wherein the core element encloses a reinforcing profile arranged within the core element.
- the fiber composite component is manufactured by a method as described.
- the fiber composite component is a fiber-reinforced body structural component or a reinforcing component of a motor vehicle.
- the body structure component may be a body pillar, in particular A, B, C or D pillar, a bow, sill, engine mount, side member, cross member, side frame or the like.
- the fiber composite component may be embodied as a reinforcing member connectable to a body structural member, such as a body pillar reinforcement, in particular an A, B, C, or D pillar reinforcement inserted between an outer and an inner side frame ,
- a reinforced fiber composite component is shown, which is configured in the illustrated embodiment, for example as a reinforcing member for an A-pillar of a motor vehicle. This can be used between an outer and an inner side frame of the vehicle.
- FIG. 2 shows a cross-section A-A of the fiber composite component 10 shown in FIG. 1 with a core element 2 braided with a sheath 3 on an outer surface 14 of the core element 12.
- the core element 12 encloses a reinforcing profile 11 arranged inside the core element 12.
- the reinforcing profile 11 integrated in the fiber composite component 10 which is arranged or enclosed within the core element 12, the component properties of the entire fiber composite component 0 are influenced and the strength increased.
- the reinforcing profile 11 it is possible to provide the reinforcing profile 11 as a tubular profile made of metal or plastic or a fiber-reinforced material and thus to increase a strength, as well as to promote an additional ductile property of the fiber composite component 10. This prevents even with large deformation paths complete tearing of the fiber composite component 10th
- the reinforcing profile 1 1 is designed as a hollow profile, which allows a high rigidity with low weight.
- the reinforced fiber composite component 10 can be produced, for example, by means of a method in which first the reinforcement profile 11 is provided and inserted, for example, into a foaming tool or an injection-molded tool (both not shown). There, the reinforcing profile 11 is foamed or overmolded with a foam material for producing the core element 12, so that the core element 12 surrounds the reinforcing profile 11.
- materials for the core element 12 are suitable for example plastic, wood, or foam material made of plastic or metal.
- the core element 12 is removed with the integrated reinforcing profile 11 from the foaming and enclosed by braiding with continuous fibers with a sheath 13.
- the braided core element 12 (including integrated reinforcing element 11) produced in this way can subsequently be impregnated with a matrix, for example by means of the resin transfer molding process.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Body Structure For Vehicles (AREA)
- Reinforced Plastic Materials (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE201310221172 DE102013221172A1 (de) | 2013-10-18 | 2013-10-18 | Verfahren zum Herstellen eines verstärkten Faserverbundbauteils |
PCT/EP2014/071604 WO2015055487A1 (fr) | 2013-10-18 | 2014-10-09 | Procédé de production d'un élément structural composite renforcé par des fibres |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3057779A1 true EP3057779A1 (fr) | 2016-08-24 |
EP3057779B1 EP3057779B1 (fr) | 2020-09-30 |
Family
ID=51691018
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP14783801.5A Active EP3057779B1 (fr) | 2013-10-18 | 2014-10-09 | Procédé de production d'un élément structural composite renforcé par des fibres |
Country Status (5)
Country | Link |
---|---|
US (1) | US20160214333A1 (fr) |
EP (1) | EP3057779B1 (fr) |
CN (1) | CN105377536A (fr) |
DE (1) | DE102013221172A1 (fr) |
WO (1) | WO2015055487A1 (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102013106070C5 (de) * | 2013-06-12 | 2019-10-24 | Leichtbau-Zentrum Sachsen Gmbh | Seitenwandgruppe für Personenkraftwagen |
CN109591508B (zh) * | 2017-09-30 | 2022-12-23 | 中山市富达运动器材有限公司 | 复合材料成形品 |
CN108481767B (zh) * | 2018-03-19 | 2021-03-16 | 航天特种材料及工艺技术研究所 | 一种相互嵌套拓扑管路类结构及整体成型方法 |
EP3802171A1 (fr) * | 2018-05-24 | 2021-04-14 | Mubea Carbo Tech GmbH | Barre stabilisatrice pour véhicule |
US11135903B2 (en) | 2019-10-17 | 2021-10-05 | Honda Motor Co., Ltd. | Method of assembling a composite side cabin structure with integrated structural core for a vehicle |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL6903871A (fr) * | 1969-03-13 | 1970-09-15 | ||
GB8316732D0 (en) * | 1983-06-20 | 1983-07-20 | Secretary Industry Brit | Zone-stiffened composites |
DE3507640A1 (de) * | 1985-03-05 | 1986-09-11 | Hubert 5778 Meschede Möller | Verfahren zur herstellung verstaerkter profilteile |
DE10158627B4 (de) * | 2001-11-29 | 2005-08-25 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Trägerstrukturen zur Aufnahme von Kräften und Verformungsenergie |
DE102004017311B4 (de) | 2004-04-06 | 2012-03-29 | Eads Deutschland Gmbh | Verfahren zum Herstellen von Faserverbund-Halbzeugen mittels Rundflechttechnik |
AT7929U1 (de) * | 2004-08-19 | 2005-11-15 | Angerlehner Hoch Und Tiefbau G | Verfahren zur herstellung eines mehrschaligen gfk-rohres und danach hergestelltes gfk-rohr |
FR2890591B1 (fr) * | 2005-09-12 | 2012-10-19 | Eads | Procede de fabrication d'une piece composite rtm et piece composite obtenue selon ce procede |
JP4263752B2 (ja) * | 2007-08-10 | 2009-05-13 | トヨタ自動車株式会社 | 繊維強化樹脂部材とその製造方法、および繊維織物の製造装置 |
FR2964339B1 (fr) * | 2010-09-06 | 2014-01-31 | Messier Dowty Sa | Procede de fabrication de pieces en materiaux composites, avec revetement tresse |
DE102010049563B4 (de) * | 2010-10-25 | 2017-09-14 | Daimler Ag | Verfahren zum Herstellen einer Drehstabfeder |
DE102010063094A1 (de) * | 2010-12-15 | 2012-06-21 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zur Herstellung eines materialhybriden Bauteils |
WO2013083172A1 (fr) * | 2011-12-05 | 2013-06-13 | Blue Wave Co S.A. | Procédé de fabrication d'un récipient sous pression utilisant une formulation prépolymère sans solvant à viscosité variable |
US9950480B2 (en) * | 2012-03-09 | 2018-04-24 | The Boeing Company | Composite structure and methods of assembling same |
CN102744889A (zh) * | 2012-07-06 | 2012-10-24 | 内蒙古金岗重工有限公司 | 碳纤维混杂树脂基复合材料泡沫夹层结构及其制备工艺 |
-
2013
- 2013-10-18 DE DE201310221172 patent/DE102013221172A1/de not_active Ceased
-
2014
- 2014-10-09 EP EP14783801.5A patent/EP3057779B1/fr active Active
- 2014-10-09 CN CN201480040897.9A patent/CN105377536A/zh active Pending
- 2014-10-09 WO PCT/EP2014/071604 patent/WO2015055487A1/fr active Application Filing
-
2016
- 2016-04-07 US US15/092,800 patent/US20160214333A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
DE102013221172A1 (de) | 2015-04-23 |
WO2015055487A1 (fr) | 2015-04-23 |
EP3057779B1 (fr) | 2020-09-30 |
CN105377536A (zh) | 2016-03-02 |
US20160214333A1 (en) | 2016-07-28 |
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